CESSNA CARAVAN AIRCRAFT 208 STRUCTURAL Repair Manual D5132-5

Cessna A Textron Company Structural Repair Manual MODEL 208 SERIES 1) Member of GAMA FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. COPYRIGHT © 1995 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1 AUGUST 1995 REVISION 5 5 MAY 2003 D5132-5-13

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL LIST OF EFFECTIVE PAGES CHAPTER-SECTION-SUBJECT Title Introduction - List of Effective Pages Record of Revisions Introduction List of Revisions List of Chapters Added PAGE DATE 1 May 5/2003 1 Mar 1/2001 2 Mar 1/2001 3 Mar 1/2001 1 May 5/2003 1 May 5/2003 INTRODUCTION - LIST OF EFFECTIVE PAGES Page 1 May 5/2003

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL INTRODUCTION 1. General A. The information in this publication is based on data available at the time of publication and is updated, supplemented, and automatically amended by all information issued in Service News Letters, Service Bulletins, Supplier Service Notices, Publication Changes, Revisions, Reissues and Temporary Revisions. All such amendments become part of and are specifically incorporated within this publication. Users are urged to keep abreast of the latest amendments to this publication through information available at Cessna Authorized Service Stations or through the Cessna Product Support subscription services. Cessna Service Stations have also been supplied with a group of supplier publications which provide disassembly, overhaul, and parts breakdowns for some of the various supplier issued revisions and service information which may be reissued by Cessna thereby automatically amending this publication and are communicated to the field through Cessna's Authorized Service Stations and/or through Cessna's subscription services. WARNING: ALL INSPECTION INTERVALS, REPLACEMENT TIME LIMITS, OVERHAUL TIME LIMITS, THE METHOD OF INSPECTION, LIFE LIMITS, CYCLE LIMITS, ETC., RECOMMENDED BY CESSNA ARE SOLELY BASED ON THE USE OF NEW, REMANUFACTURED, OR OVERHAULED CESSNA APPROVED PARTS. IF PARTS ARE DESIGNED, MANUFACTURED, REMANUFACTURED, OVERHAULED, AND/OR APPROVED BY ENTITIES OTHER THAN CESSNA, THEN THE DATA IN THE CESSNA'S MAINTENANCE/SERVICE MANUALS AND PARTS CATALOGS ARE NO LONGER APPLICABLE AND THE PURCHASER IS WARNED NOT TO RELY ON SUCH DATA FOR NON-CESSNA PARTS. ALL INSPECTION INTERVALS, REPLACEMENT TIME LIMITS, OVERHAUL TIME LIMITS, THE METHOD OF INSPECTION, LIFE LIMITS, CYCLE LIMITS, ETC., FOR SUCH NON-CESSNA PARTS MUST BE OBTAINED FROM THE MANUFACTURER AND/OR SELLER OF SUCH NON-CESSNA PARTS. B. Revisions, reissues and temporary revisions can be purchased from your Cessna Service Station or directly from Cessna Parts Distribution, Department 701, CPD 2, Cessna Aircraft Company, 5800 East Pawnee Road, Wichita, Kansas 67218-5590. 2. Coverage A. The Cessna Model 208 Structural Repair Manual is prepared in accordance with the Air Transport Association Specification 100 for Manufacturers Technical Data. B. This Structural Repair Manual contains material identification for structure subject to field repair; typical repairs applicable to structural components; information relative to material substitution and fastener installation; and a description of procedures that must be performed with structural repair, such as protective treatment of the repair and sealing. C. This manual will serve as a medium through which all Model 208 operators will be advised of actual repairs. As service records indicate a requirement, this manual will be revised to include additional specific repairs. 3. Airplane Identification A. To identify structural differences to associated airplanes, the specific airplane identity may appear in the figure and the text. Items not identified for a specific airplane or group of airplanes are suitable for all airplanes. 4. Aerofiche (Microfiche) A. The Structural Repair Manual is prepared for aerofiche presentation in addition to 8-1/2 by 11 inch loose-leaf manual format. To facilitate the use of the aerofiche, a List of Chapters with an aerofiche/ frame reference has been tabulated and incorporated into the Introduction of the Structural Repair Manual. INTRODUCTION Page 1 Mar 1/2001

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL B. Aerofiche is a microform reproduction of the contents of the 8-1/2 by 11 manual in a form convenient for service areas. An aerofiche reader is required to view the 4-inch by 6-inch aerofiche card. Each aerofiche card contains 12 horizontal rows of 24 images each. An image displays information equal to an 8-1/2 by 11 inch loose leaf page and represents a frame. Horizontal rows are lettered from A at the top to L at the bottom. Vertical columns are numbered 1 to 24. The combination of a letter and a number identifies a frame (image) in the aerofiche card. The List of Chapters provides a quick reference to information contained in the aerofiche. 5. Compact Disc (CD-ROM) A. The following manuals and service publications are available on one CD-ROM (Compact Disc - Read Only Memory): Maintenance Manual, Illustrated Parts Catalog, Structural Repair Manual, Wiring Diagram Manual, and Avionic Installation Service/Parts Manual. These publications are kept up to date through routine revisions. 6. Using the Structural Repair Manual or Aerofiche A. Division of Subject Matter. (1) Structural repair information is divided into chapters in accordance with Air Transport Association Specification 100. Each chapter is further subdivided to provide individual or related structural member presentation. (2) Chapter 51 provides general structural information required to perform a repair. Also included in Chapter 51 are general repair procedures that may be accomplished in noncritical areas. B. Effectivity Page. (1) A list of effective pages is provided with each chapter. All pages listed are active and shall appear in sequence as recorded in the List of Effective Pages. (2) The effectivity page contains tabular listing of ATA number, page and date of each page in that chapter. A change in the chapter requires a revision to the chapters List of Effective Pages. The date corresponds to the date that appears on an individual page and defines when that page was issued. C. Page Numbering System. (1) The Structural Repair Manual numbering system consists of the Air Transport Association Specification 100 three-element numbers separated by dashes. The page number and date are printed immediately to the right of the three-element number. The three-element number is assigned to a component, with the first set of numbers corresponding to ATA-100 assigned chapter number. (2) The page number complies with Air Transport Association Specification 100 for subdividing a Structural Repair Manual. Blocks of sequential page numbers are used to identify:Pages 1 Through 100 - Structural IdentificationPages 101 Through 199 - Allowable DamagePages 201 Through 999 - Repair Procedures (3) The date which appears below the page number signifies when the page was issued. If no revisions to that page have occurred, the date signifies original date. (4) Illustrations use the same figure numbering as the page block in which they appear. For example: Figure 202 would be the second figure in a repair procedure 7. Revision (Manual) A. Regular Revision. (1) Pages to be removed or inserted in the Structural Repair Manual are controlled by the Effectivity Page. Pages are listed in sequence by the three element number and then by page number. When two pages display the same three element number and page number, the page displaying the most recent Date of Page Issue shall be inserted into the Structural Repair Manual. The date column on the corresponding chapter Effectivity Page shall verify the active page. B. Temporary Revision. (1) Temporary revision pages are filed in the Structural Repair Manual by replacing existing pages in the manual. File the temporary revision cover page according to the filing instructions on the Temporary Revision Cover Page. INTRODUCTION Page 2 Mar 1/2001

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL 8. Identifying Revised Material A. Additions or revisions to text in an existing section will be identified by a revision bar in the left margin of the page and adjacent to the change. B. When technical changes cause unchanged text to appear on a different page(s), a revision bar will be placed in the left margin opposite the chapter/section/subject, page number and date of all affected pages, providing no other revision bar appears on the page. These pages will display the current revision date in the Date of Page Issue location. C. Revised text inside tables, will not display revision bars; however, the affected page will display the current revision date in the Date of Page Issue location. D. When extensive technical changes are made to text in an existing section that requires extensive revision, revision bars will appear the full length of text. E. When art in an existing illustration is revised, a hand indicator will appear in the illustration directing attention to area of the art revision. F. New art added to an existing section will be identified by a single hand indicator adjacent to the figure title and figure number. INTRODUCTION Page 3 Mar 1/2001

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL LIST OF REVISIONS 1. General A. This Structural Repair Manual includes the original issue and the following listed revisions. To ensure that information in this manual is current and the latest maintenance and inspections procedures are available, revisions must be incorporated in the manual as they are issued. Table 1. Original Issue -1 August 1995 3 September 1996 1 June 1998 5 May 2003 Writer Revision Number Date 2 4 Writer 2 September 1997 1 March 2001 jmk LIST OF REVISIONS Page 1 May 5/2003 Revision Number Date 1 3 5

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL LIST OF CHAPTERS CHAPTER Standard Practices - Structures Doors Fuselage Stabilizers Windows Wings Powerplant EFFECTIVE DATE* May 5/2003 Aug 1/1995 May 5/2003 Mar 1/2001 Aug 1/1995 May 5/2003 Jun 1/1998 FICHE/FRAME 1 A9 1 D17 1 E1 1 F12 1 G1 1 G10 1 116 NOTE 1: *Represents date of page one of each chapter's List of Effective Pages which is applicable to Manual revision date. LIST OF CHAPTERS Page 1 May 5/2003 51 52 53 55 56 57 71

CHAPTER STANDARD PRACTICES - STRUCTURES

CHAPTER-SECTION-SUBJECT 51 -Title 51-List of Effective Pages CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL LIST OF EFFECTIVE PAGES PAGE DATE 1 2 51-Record of Temporary Revisions 51 -Contents 51-00-00 51-10-00 51-11-00 51-30-00 1 2 1 2 1 2 3 201 202 203 204 205 206 207 208 209 210 211 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 9 10 11 12 13 1 2 3 4 5 6 7 8 9 51-40-00 51-40-15 Added Added Added Added Added Added Added Added Added May 5/2003 May 5/2003 May 5/2003 May 5/2003 Sep 2/1997 Sep 2/1997 Mar 1/2001 Mar 1/2001 Mar 1/2001 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 Jun 1/1998 Jun 1/1998 Jun 1/1998 Jun 1/1998 Jun 1/1998 Jun 1/1998 Jun 1/1998 Jun 1/1998 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 Mar 1/2001 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 May 5/2003 51 - LIST OF EFFECTIVE PAGES Page 1 © Cessna Aircraft Company May 5/2003

CESSNA AIRCRAFT COMPANY MODEL 208 STRUCTURAL REPAIR MANUAL 1 Jun 1/1998 2 Jun 1/1998 3 Jun 1/1998 4 Jun 1/1998 5 Jun 1/1998 6 Jun 1/1998 801 Aug 1/1995 801 Aug 1/1995 801 May 5/2003 802 May 5/2003 803 May 5/2003 804 May 5/2003 805 May 5/2003 801 May 5/2003 802 May 5/2003 801 Sep 2/1997 801 Aug 1/1995 802 Aug 1/1995 803 Aug 1/1995 804 Aug 1/1995 805 Aug 1/1995 806 Aug 1/1995 801 Jun 1/1998 802 Jun 1/1998 803 Jun 1/1998 801 Jun 1/1998 802 Jun 1/1998 51 - LIST OF EFFECTIVE PAGES Page 2 © Cessna Aircraft Company May 5/2003 51-60-00 51-70-00 51-71-00 51-72-00 51-73-00 51-74-00 51-75-00 51-76-00 51-77-00

CESSNA CARAVAN AIRCRAFT 208 STRUCTURAL Repair Manual D5132-5

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